SpaceAtlas Space Object Data
NASA JPL SBDB · 2016 NB1

2016 NB1

2016 NB1 is an Aten-type near-Earth asteroid whose orbit lies mostly inside that of Earth, with a semi-major axis of 0.762 AU and a period of 0.67 yr.

Aten Observations: 117
Orbital Period · P
0.67 yr
v(q)
54.3 km/s
v(Q)
21.4 km/s
Diameter · ≈
0.06 km
TJ
7.51
Eccentricity · e
0.4351

Orbit and dynamics

The path is an ellipse reaching 0.431 AU from the Sun at perihelion and 1.094 AU at aphelion, a radial span of 0.663 AU.

Applying Kepler's third law to a = 0.762 AU gives an orbital period of 0.67 yr, or about 243 days.

The high eccentricity (0.435) produces a strongly elongated orbit, so the object spends most of its time far from the Sun.

The orbital plane is tilted 6.68° relative to the ecliptic.

By the vis-viva equation its orbital speed rises to 54.3 km/s at perihelion and falls to 21.4 km/s at aphelion.

Because q < 1 AU and Q > 1 AU, this orbit geometrically intersects the region of Earth's orbit.

Size and surface

No direct size measurement is available; from an absolute magnitude of H = 23.9 and an assumed geometric albedo of 0.14, the diameter works out to roughly 0.06 km.

Observation record and orbit quality

The current orbit solution is based on 117 observations and has a weighted RMS residual of 0.4041 arcseconds.

Condition code U = 1 means the orbit is very well determined, leaving only a small uncertainty in the future ephemeris.

About these computed values

Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Orbital Parameters

Semi-Major Axis
0.7624 AU
Eccentricity
0.4351
Perihelion
0.431 AU
Aphelion
1.09412 AU
Inclination
6.68°
Orbital Period
— yr
Epoch
2461200.5
Mean Anomaly
123.86°

Orbit diagram

The Sun sits at the focus (orange). Earth's orbit is the grey circle at 1 AU. The red dot marks the object's position at the catalog epoch.

3D orbit (interactive)

Drag to rotate; scroll or pinch to zoom. The Sun is at the focus (orange), Earth's orbit is the grey ring at 1 AU, and the red dot marks the object's current position.

Close approaches

Predicted close approaches to Earth, from NASA's Center for Near-Earth Object Studies (CNEOS).

Date (UTC)Miss distanceVelocity
2028-Jul-17 10:26 0.077506 AU
11594684 km
8.43 km/s
2030-Jul-21 09:20 0.076265 AU
11409010 km
8.43 km/s
2032-Jul-24 10:17 0.073621 AU
11013547 km
8.46 km/s
2034-Jul-28 04:15 0.069808 AU
10443066 km
8.52 km/s
2036-Jul-30 20:08 0.064822 AU
9697292 km
8.62 km/s
2038-Aug-03 06:46 0.059368 AU
8881319 km
8.79 km/s
2040-Aug-05 09:53 0.054312 AU
8124909 km
9.02 km/s
2042-Aug-08 01:08 0.051221 AU
7662586 km
9.31 km/s
2044-Aug-09 08:06 0.051206 AU
7660288 km
9.67 km/s
2046-Aug-11 08:21 0.056383 AU
8434817 km
10.17 km/s
2048-Aug-12 01:19 0.069420 AU
10385062 km
10.88 km/s
2050-Aug-13 06:55 0.091051 AU
13620977 km
11.79 km/s
2052-Aug-12 22:18 0.118641 AU
17748487 km
12.81 km/s
2054-Aug-13 03:06 0.150099 AU
22454495 km
13.92 km/s
2056-Aug-11 23:24 0.185182 AU
27702875 km
15.15 km/s

Distances in astronomical units (AU) and kilometres. Source: NASA/JPL CNEOS Close Approach Data API.

Physical Parameters

Diameter
— km
Albedo
—
Density
— g/cm³
Rotation Period
— h
Absolute Magnitude
23.9

Orbit Quality

RMS
0.40408
Condition
1
Orbit ID
—
Data source: NASA JPL Small-Body Database · NASA CNEOS. Orbital periods, perihelion and aphelion speeds, and diameter estimates on this page are computed by SpaceAtlas from the JPL SBDB orbital elements. They are derived quantities, not values copied from the source catalogue.

Keep exploring

Explore asteroids, comets and near-Earth objects with JPL orbital data.